US2938431A

US2938431A - Latch mechanism for a 3.5" rocket launcher

Info

Publication number: US2938431A
Application number: US769522A
Authority: US
Inventors: Paul H Dixon
Original assignee: Individual
Current assignee: Individual
Priority date: 1958-10-24
Filing date: 1958-10-24
Publication date: 1960-05-31
Anticipated expiration: 1977-05-31

Description

May 31, 1960 P. H. DIXON 2,933,431

LATCH MECHANISM FOR A .5" ROCKET LAUNCHER Filed Oct. 24, 1958 3 Sheets-Sheet l I lllnl 7 PFIUL $910M. 5 INVENTOR.

May 31, 1960 P. H. DIXON LATCH MECHANISM FOR A 3.5" ROCKET LAUNCHER Filed Oct. 24, 1958 3 Sheets-Sheet 2 F401. M XON.

IN V EN TOR W am aam ay 31, 1960 P. H. DIXON 2,938,431

LATCH MECHANISM FOR A 3.5" ROCKET LAUNCHER Filed Oct. 24, 1958 3 Sheets-Sheet 3 v mm Patented May 31, 1960 LATCH MECHANISM FOR A 3.5" ROCKET LAUNCHER This invention relates to a latch mechanism for a 3.5 -rocket launcher and more particularly to a contact latch mechanism serving to position and hold'a rocket in its firing position in a rocket launching tube and to make :automatic electrical contact with the electrical firing .source.

It is a primary object of this invention to provide a llatch mechanism to position a rocket in a launching tube :for firing therein.

Itis another object to provide an automatic electric ifiring means disposed between the rocket contact band and the firing circuit.

It is another object of the invention to provide a latch mechanism for a rocket launcher that will automatically ;.raise the latch and stop levers out of'the path of a rocket ;blast to prevent their deterioration or injury therefrom.

It is a still further object of the invention to provide 7 :a latch mechanism for a rocket launcher that is fully :automatic in operation to permit rapid ,launching of zl'OCkGtS therefrom and to permit a quick removal of rmisfires from the launcher.

The specific nature of the invention as well as other objects and advantages thereof, will clearly appear from -.a.description of a preferred embodiment as shown in the .accompanying drawings in which:

.Fig. 1 is a top plan view of a latch mechanism con- :structed in accordance with the invention and afiixed to the breech end of a rocket launching tube;

.Fig. 2 is a side elevation of the latch mechanism;

Fig. 3 is a frontal view to an enlarged scale of the 'latch mechanism, the breech guard being broken away :to reveal the mechanism;

Fig. 4 is a sectional view taken along the line 44 -of Fig. 3, looking in the direction of the arrows and illustrating the latch mechanism in plan;

Fig. 5 is a sectional view taken along the line 55 of Fig. 3, and looking in the direction of the arrows;

Fig. '6 is sectional view taken along the line 6-6 of Fig. 4 and looking in the direction of the arrows, a rocket tail being shown in its firing position within the launching tube,

Fig. 7 is a similar view to Fig. 6, but showing the slide being released and the latch and stop levers being in raised position out of the path of the rocket blast;

Fig. 8 is a sectional view taken along the line 88 of Fig. 4 and looking in the direction of the arrows;

Fig.9 is an enlarged detail cross sectional view of the contact button;

Fig. 10 is an enlarged horizontal sectional view of the cam and plunger; and,

Fig. 11 is a perspective view of the loaders safety slide.

Referring more particularly to the drawings in which like reference characters designate like parts throughout the several views reference character 1 indicates generally -the breech end of a rocket launcher and includes a tube 2 and a breech guard 3. An opening 4 is provided in the breech guard to permit the entrance of rocket indexing members, to be described.

Afiixed to the rearward portion of the breech end of the launcher is a housing indicated generally by 5 and includes a front wall 6, side walls 7 and a topwall 8. The top wall 8 is provided with an opening 9 for access into the housing and is covered by a lid 10.

The operating elements of the latch mechanism are mounted within the housing 5 and include an elongated latch lever indicated generally by 11, Lever 11 is con.- structed of a pair of

side members

12 and 13 joined medially along their top edges by an integral web pontion 14. (See Fig. 4.)

Side members

12 and 13 are bored as at 15 at their forward ends thereof to receive a bushing 16. When assembled, this bushing receives a pin 17 trunnioned in side walls 7 of housing 5 trans.- versely of the longitudinal axis of the launcher, provid ing a pivot for the lever 11. The rearward ends of

side members

12 and 13 are attached by suitable means such as welding, to a block 18 defining a latch portion 19,. The latch 19 defines a beveled rearward surface 20 and a vertical forward surface 21 for a purpose to be later described. A coil torsion spring 22 is disposed around pin 17 between side member 12 and a side wall 7 of housing 5. One end of spring 22 is received in a notch 23 in side wall 12, while the other end bears against top wall 8 of housing 5, normally biasing lever 11 downward and through opening 4 so that latch 19 may engage a rocket contact band A of a rocket R when in tube 1. (See Fig. 6.) The latch portion 19 is further beveled as at 24 (see Fig. 3) to prevent a rocket fin-from bearing against the lever 11 and preventing its entrance into the launching tube. Block 18 is bored as at 18 to receive a contact button 26. Contact button 26 is insulated from block 18 by a bushing 27 and a washer 28 both of a dielectric material. A rocket stop lever, indicated generally by 25, is pivotally mounted between

side members

12 and 13 by pivot pin 25 and is disposed forwardly of latch 19 (see Fig. 8). The upper portion of stop lever25 is milled out as at 27 forming a pair of upstandingears. A pin 25 transversely pierces these ears and extends into a pair of arcuate slots 29 formed in

side members

12 and 13 of lever .11, limiting the rotation of stop'lever 25. The lower portion of stop lever 25 is beveled as at 30 to prevent engagement of a rocket fin and preventing indexing of the rocket. A vertical rearward face 31 of 25 is provided to engage the contact ring A of a rocket R. (See Fig. 6). A coil spring I contact ring A and prevents forward movement of the rocket R in tube 2.

Means for making electrical contact between the rocket contact ring A and the trigger circuit (not shown) is provided and consists of substantially U-shaped slide member indicated generally by 34. This slide is illustrated in perspective per se in Fig. 11 and comprises a pair of rearwardly extending

arms

35 and 36. A portion of the frontal end is turned back upon itself to form a loop 37 to provide a handle for the loader in manipulating the mechanism. The inner edges of the arms are turned up as at 38 to provide a pair of runners which slide in a pair of slots 39 provided in the front wall 6 of housing 5. Slide 34 is arcuate in cross section and is adapted to slide along the outer peripheral surface of tube 2 and is guided into housing 5 by the slots 39. A block 40 is carried by the rearward portion of arm 35 and normally rides under a turned down portion 41 of top wall 8 (see Figs. 3 and 5) which serves to keep the slide close to the tube 1 for a purpose that will be readily apparent as the description progresses. A first bracket 42 is carried by a side wall 7 (see Fig. 3) and a second bracket 43, in alignment with the first bracket 42, is carried by arm 35 of slide 34." A guide rod 44 is supported at its ends in

brackets

42 and 43 and a coil spring 45 encircles rod, 44 and bearing against

brackets

42 and 43 normally tends to bias the slide in a forward direction. Provision is made for thepassage of rodl42 *and spring 45 through block 40 by longitudinal bore 46in the block. [A U. -shaped switch operating membe'r 47 is provided on the rearward portion of arm 36 ofslide 34 (see Fig. 11) the function of which is to be described later. Meansfor lifting the latch lever 11 and ,itsstop lever 25 out of the, path of rocket blast iscarried by theflateh lever and the slide and cooperate to lock the slide in its cocked position when pushedin.

Its upper edge is flush withthejupper' edge of side member 13, Cam 48-defin'es abevele'd

forward edge

49,5 vertical rearward edge 50 and art inclined lower edge j serves to hold the contact button 26, bushing 27 and washer 28 in assembled relation in block 18. An insulating'plate 57 serves to insulate the connection from metallic parts of the lever. A first lead 55 is connected to a switch 58 carriedby the inner surface of one side wall 7. A button 59 (see Fig. 3) operates the switch and is carried by the under-part of switch 58 and lies in the path of member 47 on arm 36 of slide 34. Switch 58 is connected by a second lead 60 to atrigger mechanism not shown. A third lead 6'1'provides aground connection from'the latch lever 11 to the latch housing 5.

As the -firing circuit, not shown, is connected to the contact button, no wires are necessary to connect before arming the rocket in the tube 2. A live rocket R is inserted into the tube 2 until the, forward edge of the rocket contact band support ring A abuts the rearward vertical face 31 of the rocket stop lever 25 which will prevent further forwardmovement of the rocket into the tube 2. The rear edge of the support ring A will be engaged by the vertical face'21 of the latch portion 19. Thus the rocket R 'will be prevented fromsliding out from the rear of th'etube 2. Whenthe rocket Risinserted into the tube 2, thewarhead, not shown, and the contactband supportA will'ride easily underthe stop lever 25 and latch portion19yas they will be pushed upwardly against the bias of torsion spring 22 and coil spring 32. The upward movementof lever 11 is made possible by the rearward beveled face '20 of latch 19 and the rotation of stop lever 25 against the pull of coil spring 32. This forward rotationof stop lever 25 is limited to the necessary movement to clear the latch and stop levers from the rocket blast by arcuate slots 29' and pin 26 Thus, a smooth and rapid loading of the tube is possible. When the rocket R is held between the latch portion 19 and the stop lever 25, contact button 26 will bear on the electrical contact band B of the rocket. Due to torsion spring 22, positive electrical contact ismade as long as the rocket is in this position. Beveled surfaces 24 on latch19.an d 30 on stop lever 25 will prevent hang" of the'rocket during loading by a fin, as when a fin strikes are 'of,these beveled surfaces, it will be,v rotated out of the way. The rocket is now ready for arming. Arming isv accomplished by moving the loaders slide 34 rearwardly approximately one and nine sixteenths inches, or

until the time delay plunger 52, which is carried in block,

40cm arm 35 of slide 34 is moved to the rear of cam plate and snaps over. the vertical edge, whence, the

A cam plate 48;,is' affixed to the outer side of side member 13 of the latch, lever -11 andis disposed substantially medially thereof.

rearwardly, the plunger 52 will be moved inwardly by the beveled edge 49 and'will'be held thus'until-reaching the end of the plate 48. At the same time, the member 47 will be moved under the button 59 of switch 41 which will close the switch to establish electrical contact between the trigger (not shown) and the rocket. As the circuit is grounded when the rocket is in the tube, it is now ready to be fired.

Actuating a trigger mechamsrmnot shown, ignites the rocket. The tensionof coil spring 45 is such thatwhen, the rocket attains a thrust of approximately nineteen' pounds, the stop lever 25 will be raised and at the same time the latch lever 11 will lift upwardly to bring the delay plunger 52 down under the angled lower edge 51 of cam plate 48 and release slide 34. tomove forward. As the'slide' moves forward under the inclined edge 51 of cam 48, the plunger will raise the latch lever 11 up- ;wards sufiiciently to remove the stop. lever..25 and the latch 19. out of therocket blast path (see Fig. 7). When n the slide 34 reaches its v full'for vardposition, the plunger; will resume its positionin front of the cam. plate 48.

Also, the circuit willbe broken by the member 47 mov ing away from button 59 of switch 41 and the launcher will be in safe or uncocked condition.

From the foregoing description, it is apparent that a more eflicient latch mechanism has been devisedthat. will enablethe operator tomore quickly and safely load, unload and fire rockets from the launcher. In case of a misfire, allthat is necessary to do to unload the rocket": is to push or pull slide 34 forwardto break the'finngv circuit. Then the safety switch. on. the trigger mechanism (not. shown) 'ma be moved to its safe position.

The slide 34 is then pushed to its full rearward position into thehousing 5 and then pulled out sufiiciently for theplunger152 to lift lever 11. The slide 34 is heldhere N in this position and the rocket maybe removed from the 7 tube and 'disarmed.

While a preferred form of -the invention has been shown and described,.various modifications and substitutions of equivalents will occurto. those skilled in the art after a study of the foregoing disclosure. Hence, the

disclosure should be taken in an illustrative rather than a limiting sense, and it is thehdesire and intention to reserve all modifications with the scopeof the subjoined claims. What is claimed is:

1. In a latch'm I ham'sm for a rocket launcher, a rocket launchingtube having an openingadjacent its breech, end thereof, a housing secured to the breech end of said tube and over saidopening, said housing including apair of side walls, a' front wall and a top wall, a springloaded latch lever pivotallymounted at its forward end, to said side-walls ofjsaid 'housing, the rearward end of said latch "lever normally extending through said opening.

and into said launching tube, a. spring loaded rocket stop lever carried by ,the rearward, portion of. said latch, lever forholding a rocket in its firing position 1n 331d launching tube, an electrical contact button carried by the rearward end of. said latch lever adapted to contact the contact band 'of. a rocket when in firing position insaid launching tube, a contact switch carried by one of-said side walls ofs aid housing, a spring-loaded slide member defining a' pair of 'rearwardly extending arms adapted to slide along the outer peripheral surface of. saidlaunching tube andinto said housing, alcam plate carried by one side of said latch lever, a spring-loaded,plunger care ried by one arrnofsaidslide, a switeh operating member carried by the other arm of said-slide member, said.

slide member, said plunger, said carn pl te and sai switch operating member functioning, when said' slide ispushed all the .way into said housing, to lockjsa'id slide in its rearwardposition an'd' to close said switch, and electrical connections between said contact button,

said switch and a firing means comprising a first elee tripallead qnnqgt fig-se f q aabut it ffisis swi sht a second electrical lead connecting said switch to a firing means and a third electrical lead grounding said switch to said housing.

2. A latch mechamm for a rocket launcher including a rocket launching tube having an opening therein adjacent its breech end and a housing securing to said breech end of said tube and over said opening, means for holding a rocket in firing position in said tube comprising, an elongated spring-loaded lever substantially channelshaped in cross section, pivoted at its forward end in said housing, said lever being disposed in a parallel relation with respect to the longitudinal axis of said tube, its rearward end normally extending through said opening and into said tube, said rearward end defining a latch portion adapted to engage the rearward edge of a rocket band supporting ring of a rocket when said rocket is in the firing position within a tube and prevent rearward displacement thereof, a spring-loaded stop lever pivotally mounted on said elongated spring-loaded lever and spaced forwardly of said latch portion and in longitudinal alignment therewith, said stop lever adapted to engage the forward edge of the contact band supporting ring on the aforesaid rocket when it is in the aforesaid firing position in said tube to prevent forward displacement thereof, an electrical contact button carried by said elongated springloaded lever and disposed between said latch portion and said stop lever and in longitudinal alignment therewith, said button normally contacting a contact band of a rocket when said rocket is in its firing position in said tube, means raising said latch lever upon forward move ment of said slide comprising, a cam plate, defining an inclinded under edge, a vertical rearward edge and a beveled forward edge, secured to one side of said latch lever, a spring-loaded slide member adapted to slide on the outer peripheral surface of said tube and into said housing, a spring-biased plunger carried by said slide member and being disposed transversely with respect to the longitudinal axis of said tube, said plunger being normally biased against the side of said elongated lever and adjacent the beveled edge of said cam plate, said plunger, upon rearward travel of said slide to snap over said vertical edge of said cam plate and lock said slide in a full rearward position, said stop lever to be lifted by forward passage of said contact band supporting ring upon firing of said rocket in said tube and release said plunger to allow said slide to move in a forward direction, said plunger riding under said inclined edge of said cam plate and lift said elongated lever upwardly to remove said latch portion and said stop lever from said tube, a firing circuit connecting said contact button to an electrical firing source, a contact switch mounted in said housing and in said circuit, and means carried by said slide cooperating with said switch to close said switch upon locked position of said slide and opening said switch upon release of said slide to said forward position.

3. A latch mechanism for a rocket launcher as described in claim 2 wherein said cam plate and said springbiased plunger coact upon forward movement of said slide to provide a time delay of sufficient duration for said lifting of said elongated lever whereby said latch portion and said stop lever is removed from said tube to allow escape of blast gases in said tube from a rocket fired therein.

4. In a latch mechanism for a rocke launcher as described in claim 2 wherein said slide comprises a U-shaped member defining an arcurate cross section and a pair of rearwardly extending arms, one of the arms carrying said spring biased plunger and the other am said switch operating member.

References Cited in the file of this patent UNITED STATES PATENTS 2,460,929 Goff Feb. 8, 1949 2,751,818 Bonnett June 26, 1956 2,764,066 Doak et a1. Sept. 25, 1956 2,830,496 Anderson et a1 Apr. 15, 1958 2,836,105 Doak et al. May 27, 1958